23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5638940969880548---------------------------
|
|
|
|
Spacecraft: mySat
|
|
dry_mass: 200.0 kg
|
|
specific impulse: 3200.0 kg/s
|
|
max_thrust: 0.00025 kN
|
|
num_thrusters: 1
|
|
duty_cycle: 1.0
|
|
Launch Mass: 3500.0 kg
|
|
Launch Date: 2024-05-08T23:01:40.501
|
|
Launch V∞: [7.965689808391153, -5.802036155013386, 0.06010456358330123] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [2.0235823388995987e-8, -1.866525265237025e-7, 9.236411877434769e-9] km/s
|
|
V∞_out: [-2.7388026806085997e-8, 1.1311976711625465e-7, 1.4916318846536598e-7] km/s
|
|
time of flight: 1.76329289034966e8 seconds
|
|
arrival date: 2029-12-09T19:23:09.501
|
|
thrust profile: [0.3059845131104925 -0.019588625411603992 -0.0925377681494782; 0.06231855551576348 0.03239640156705868 -0.06332115972999187; 0.0391945699042798 0.03436982671455866 -0.07084604379519847; 0.04570478980419496 0.05336522740798875 -0.11860997986128488; 0.04416634307990966 0.06351458962187927 -0.15198399655024242; 0.05911042845066327 0.09816331090701363 -0.2443384628332286; 0.006746233217213406 0.013172721029529436 -0.03770321478529659; 0.0033801012378431717 0.007225238562728068 -0.02159269845337054; 0.0023045344276111076 0.00530166830249452 -0.01745829103428388; 0.010214846392750247 0.027257039539902748 -0.08379651033502197; -0.00041290196061306026 0.00017949763331707568 -0.001182311552060476; -0.0002173634103738763 0.002446279027270713 -0.004396523743183392; 0.0010859485049511562 0.0011654738660525363 -0.004174383331769484; 0.0005181917102231894 0.0008454067220334555 -0.0028319127787348264; 0.0015451057351421249 -0.0024145158293730996 -0.0023842124465000315; -0.0003258623428074787 -0.007504444396168987 -0.004499224679447831; -0.0008730565663721988 -0.00042776840822062183 0.0060539842338458855; -0.006986212151885525 -0.005857563894522086 -0.0013521423336076217; -0.0002002951456262865 0.0016063419837540616 -0.0003523651672477534; -0.0008995385576803662 -0.0002802461824413671 0.0059735578288356225] %
|
|
|
|
Mass Used: 91.34632016683963 kg
|
|
Launch C3: 97.11945022615275 km²/s²
|
|
||V∞_in||: 1.8797331063287075e-7 km/s
|